19980304002569A

Accident · Destroyed

FAA accident report · Cessna 150M · Haverhill, MA · March 4, 1998

Date
March 4, 1998 · 09:06 local
Place
Haverhill, MA
Phase of flight
Fcd/Prec Ldg From Cruise
Operating rules
General operating rules (Part 91)
Damage
Destroyed
Aircraft
N63387
NTSB investigation
NTSBIAD98LA034
Reported as
Cessna 150M
Reported engine
Continental O200A
People aboard
3
Fatal injuries
0
Pilot’s flight hours
1,520 total900 in this make and model180 in the last 90 days

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

Acft exper a rough running engine, made an emergency landing at old dutton arpt. Ran off end of rwy. (.4)in level flight at 2,000 feet, the engine began running rough with an associated vibration. The CFI took control of the airplane and the vibration became stronger. After shutting down the engine, the CFI attempted to land on an abandoned runway. The airplane impacted trees approximately 100 feet beyond the departure end of the abandoned runway. Examination of the engine logbooks and discussions with the operator disclosed that the engine was 362 hours beyond time between overhaul (tbo) and automotive fuel was utilized without a supplemental type certificate. Disassembly of the engine revealed the number two cylinder's exhaust valve was fractured and the cylinder was cracked. An examination of the fractured exhaust valve by the materials laboratory division of the national transportation safety board revealed that the 'shank area immediately adjacent to the fracture was reduced in size, and the fracture features were indicative of bending overstress separation with no indications of pre-existing cracking.' (-23) engine failure. Exhaust valve stem elongated then failed near head. Catastrophic damage to piston and cylinder.

As the FAA filed it

ACFT EXPER A ROUGH RUNNING ENGINE, MADE AN EMERGENCY LANDING AT OLD DUTTON ARPT. RAN OFF END OF RWY. (.4)IN LEVEL FLIGHT AT 2,000 FEET, THE ENGINE BEGAN RUNNING ROUGH WITH AN ASSOCIATED VIBRATION. THE CFI TOOK CONTROL OF THE AIRPLANE AND THE VIBRATION BECAME STRONGER. AFTER SHUTTING DOWN THE ENGINE, THE CFI ATTEMPTED TO LAND ON AN ABANDONED RUNWAY. THE AIRPLANE IMPACTED TREES APPROXIMATELY 100 FEET BEYOND THE DEPARTURE END OF THE ABANDONED RUNWAY. EXAMINATION OF THE ENGINE LOGBOOKS AND DISCUSSIONS WITH THE OPERATOR DISCLOSED THAT THE ENGINE WAS 362 HOURS BEYOND TIME BETWEEN OVERHAUL (TBO) AND AUTOMOTIVE FUEL WAS UTILIZED WITHOUT A SUPPLEMENTAL TYPE CERTIFICATE. DISASSEMBLY OF THE ENGINE REVEALED THE NUMBER TWO CYLINDER'S EXHAUST VALVE WAS FRACTURED AND THE CYLINDER WAS CRACKED. AN EXAMINATION OF THE FRACTURED EXHAUST VALVE BY THE MATERIALS LABORATORY DIVISION OF THE NATIONAL TRANSPORTATION SAFETY BOARD REVEALED THAT THE 'SHANK AREA IMMEDIATELY ADJACENT TO THE FRACTURE WAS REDUCED IN SIZE, AND THE FRACTURE FEATURES WERE INDICATIVE OF BENDING OVERSTRESS SEPARATION WITH NO INDICATIONS OF PRE-EXISTING CRACKING.' (-23) ENGINE FAILURE. EXHAUST VALVE STEM ELONGATED THEN FAILED NEAR HEAD. CATASTROPHIC DAMAGE TO PISTON AND CYLINDER.

NTSB investigation

The NTSB’s investigation of this event, with its probable cause and findings. Matched to this report by N-number and date.